| Alternative title | Rapport d'essai de vibration de l'articulation à rotule entre le Module cible canadien (MCC) et le matériel de soutien aéroporté |
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| Download | - View final version: Canadian target assembly (CTA) to airborne support equipment (ASE) vibration test report (PDF, 27.0 MiB)
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| DOI | Resolve DOI: https://doi.org/10.4224/40003111 |
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| Author | Search for: Ross, J. E.1 |
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| Affiliation | - National Research Council of Canada
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| Format | Text, Technical Report |
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| Physical description | 58 p. |
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| Abstract | This report documents the full flight vibration load testing of the CTA to ASE Ball and Socket joint (CABS), which has been designed and built by the Advanced Manufacturing Program and Flight Research design offices and workshops here at the National Research Council Canada (NRCC). This program has been run jointly by the Canadian Space Agency (CSA) and the NRCC. The testing has been done to meet the requirements of the NASA interface control document ICD-A-21056 for shuttle orbiter/CANEX -2 interfaces.
The tests were conducted at the David Florida Laboratory (DFL) from 1 to 11 April 1992. This laboratory is associated with the CSA. |
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| Publication date | 1992-12 |
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| Publisher | National Research Council of Canada. Institute for Mechanical Engineering |
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| Series | |
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| Language | English |
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| Peer reviewed | No |
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| NRC number | NRCC 33592 |
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| Export citation | Export as RIS |
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| Report a correction | Report a correction (opens in a new tab) |
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| Record identifier | f473a18e-2f1b-4b55-b9f1-13a7fca53555 |
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| Record created | 2023-07-25 |
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| Record modified | 2023-07-25 |
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